REFLECTOR: Electrical system

Chris Barber cbarber at texasattorney.net
Thu Jul 4 18:48:23 CDT 2013


Reiff,

Just as a basis of comparison, Bob Knuckles, on his Aeroelectric.com<http://Aeroelectric.com> site, does a point by point critique of Richter's paper. IMAO, he attempts to educate and explain the various factors. The write up is available on the site and may provide insight so you may make a more well informed choice.

Just FYI.

Chris
Houston

Sent from my iPhone 5

On Jul 4, 2013, at 15:07, "Reiff Lorenz" <Reiff at Lorenz.com<mailto:Reiff at Lorenz.com>> wrote:


Larry,

Thanks for the link. Just read through the whole thing.

Did you follow this advice? One battery, one alternator, 24 volts? Do you have any backup systems, like vacuum pump instruments or in-EFIS batteries? What about electronic ignition?

I'm fascinated to hear what other builders are doing. It's a big help when considering the options for my installation.

Thanks!

Reiff




From: reflector-bounces at tvbf.org<mailto:reflector-bounces at tvbf.org> [mailto:reflector-bounces at tvbf.org] On Behalf Of Lawrence Epstein
Sent: Thursday, July 4, 2013 1:52 PM
To: Velocity Aircraft Owners and Builders list
Subject: Re: REFLECTOR: Reflector Digest, Vol 100, Issue 10

I strongly recommend the following reference for aircraft wiring/electrical systems:

http://www.eaa.org/experimenter/articles/0903_aircraft_wiring.pdf

Granted, it is written by Greg Richter (BMA), but it goes through a logical analysis of what sort of redundancy is necessary and where. He addresses back up batteries (no need if you are 24 V) on page 5 and 2nd alternator ("overkill") on page 6.

Lots of good stuff here.

On Thu, Jul 4, 2013 at 11:15 AM, Patrick Sieders <pjsieders at comcast.net<mailto:pjsieders at comcast.net>> wrote:
Brooke and Dave,

You all have a point in simplicity. On backup systems however, I disagree.

Many production airplanes had backup systems : electrical and suction instruments.

These days we are all leaning/using electrical EFIS screens etc. So to have another backup alternator in lieu of the old vacuumpump is just common sense.

Take it from a guy flying an electric airliner, being told we always will have instruments(i.e. EFIS SCREENS) to look at.. I have met Murphy in IMC...

Patrick sieders


________________________________
From: Dave T Nelson <dtnelson at us.ibm.com<mailto:dtnelson at us.ibm.com>>
Sent: July 04, 2013 10:09
To: reflector at tvbf.org<mailto:reflector at tvbf.org>
Subject: Re: REFLECTOR: Reflector Digest, Vol 100, Issue 10

Brooke - well said, Sir!

The comparison to other no redundancy systems (like your entire airframe) is spot on, and reinforces my philosophy - stay away from complexity, and build it really, really well - but just once.  Adding all the stuff I hear about is adding extra weight, complexity, and failure modes.

How many Cessnas, Pipers, Beechcrafts, Mooneys, etc., are lost due to the lack of an extra alternator?  An extra battery?  Where you see a store bought airplane accident due to an electrical failure, it's pretty much always due to smoke or fire in the cockpit... How much extra risk are you adding for that kind of problem with all of your additional redundant systems?

Take great care in building, but build it once and keep it simple.

Dave

Dave T. Nelson
T/L 553-4327, Voice 507-253-4327<tel:507-253-4327>, Fax 507-253-3648<tel:507-253-3648>
Program Director, ISC ECAT NPI & Test Engineering

----- Message from Brooke Wolf <bwolf1 at tds.net<mailto:bwolf1 at tds.net>> on Wed, 3 Jul 2013 21:32:32 -0400 -----
To:

reflector at tvbf.org<mailto:reflector at tvbf.org>

Subject:

REFLECTOR: Electrical system

Reiff

As we go through the mental gymnastics of 2 alternators or 2 batteries or primary busses or essential busses or main busses or emergency busses or battery busses and redundancy galore, let us not forget we have only one engine.  Safety and associated redundancies should balance.  Just food of thought.

Brooke

On Jul 3, 2013, at 4:11 PM, reflector-request at tvbf.org<mailto:reflector-request at tvbf.org> wrote:
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Today's Topics:

 1. Re:  Electrical system (Jack Prock)

From: "Jack Prock" <jackprock at wavecable.com<mailto:jackprock at wavecable.com>>
Subject: Re: REFLECTOR: Electrical system
Date: July 3, 2013 4:10:30 PM EDT
To: "Velocity Aircraft Owners and Builders list" <reflector at tvbf.org<mailto:reflector at tvbf.org>>
Reply-To: Velocity Aircraft Owners and Builders list <reflector at tvbf.org<mailto:reflector at tvbf.org>>


Reiff,

The only thing that I would add is that you start your engine using the battery, but fly using your alternator(s).  If you were going
to decide between having a duplicate of one OR the other, I would go with a duplicate alternator.

If the battery goes out, you can’t start... get jumper cables, start the engine, you’re on your way... just like a car. (assuming 12 volt system )

If your single alternator goes out, you run on your battery(s) until it/they die (while you look for a place to land)...
at night... over mountains, not a good scenario!!  Other backups will help... but the pucker factor goes way up when
(almost) everything goes dark!

The consequences of one, far outweigh the consequences of the other.

That is just my opinion... and just like assholes, everyone has one!!

Jack

From: Reiff Lorenz<mailto:Reiff at lorenz.com>
Sent: Wednesday, July 03, 2013 12:24 PM
To: Velocity Aircraft Owners and Builders list<mailto:reflector at tvbf.org>
Subject: Re: REFLECTOR: Electrical system


Terry,

Thank you for all the details. This is all very helpful. I like your suggestion about the heat-shrink labeling, even though it's expensive. For planning/drawing software I'm leaning toward Visio. (Turbo-CAD does have some good features, too.)

I'm still working on the right tradeoff between redundancy and complexity. Lots of suggestions from other builders to do 2 batteries. Others say 1 battery and 2 alternators. Andy Millin sent me his diagram and he's got 3 batteries! The Vertical power system simplifies some of this. They have multiple configurations for dual batteries and/or dual alternators and/or ground power plugs, but it's still not as easy as connecting everything to one box.

Builder Bill Stockman lives near me. He's retro-fitting his long-wing SE with a Vertical Power system and a Garmin G3X. I'm hoping to be able to help him and learn about wiring a VP system in the process.

I may have similar W&B issues to what you describe. I'm a skinny guy and don't want to have trim issues, but I also want to take some of my larger friends in the front seat (6'3 & 260 lbs.)  Maybe there's some middle ground between the two extremes?

Looking forward to talking to you at Oshkosh!

Reiff


From: reflector-bounces at tvbf.org<mailto:reflector-bounces at tvbf.org> [mailto:reflector-bounces at tvbf.org] On Behalf Of Terry Miles
Sent: Tuesday, July 2, 2013 11:46 PM
To: Velocity Aircraft Owners and Builders list
Subject: Re: REFLECTOR: Electrical system

Wow.  Dave, that is a very nice summary.  I did all of my wiring...every inch, every connector, every everything.  I would repeat a lot of what you offered, if asked, and that is:  keep track of wire size to fit the current load, secure stuff properly so it cannot rub against anything,  (I used that black wax lace stuff.  Yank on every connector after you make it to test it.   Check every BNC you make for continuity and twist it around a little before you declare it sound.   If you make 25 pin connectors becareful with pin crimps, and especially the outboard most pins when you go to secure the entire bundle.  (You can google how to tied the knots.)  I read all the Nuckols stuff faithfully as I educated myself and choose against the double alternators, but I do have a pair of Odessey 925 batteries located forward of the carnard bulkhead in the RG and have not had water issues so far.   The main distribution is after of the carnard bulkhead.   I did the 2 batts in part for wgt and bal since I am 150 pounds and heard stories of trim issues.  While it is another discussion,  the decision for one or two batts was and always will be debatable.  It might have been better for me to use removable ballast since I cannot take anybody much over 200 lbs and put them in the front seat.  My inflight draw is about 4 amps, much much different from days gone by.  I will run out of gas before I every run out of batt power.  I replace one batt every 18 months to two years.

Making wire streams (I like that term) would have been some good advice for me.  I didn't do that and actually installed the wiring a little at a time and added a lot of after the fact stuff....and I do have a lot of loose single wires going hither and yon (sp?) back and forth from port to starboard behind the instrument panel.  I used auto fusing mostly but do have about a dozen in view aircraft grade CB's for stuff I want to know about...ignition, transponder, hydro pump and gear control gizmo...stuff like that.  There are also decisions about putting more than one component into a single fuse/breaker.

I bought a $300 plus wire labeling system that uses heat shrink.  The dam heat shrink refills were about 35 cents an inch, but I thought that was money well spent, as well as being able to work at a base level with turbo-cad to do the drawings since I experienced endless edits in that department from my first paper drawings.

If you do your own wiring, I would call Dave first since he offered.  I am only a Saturday afternoon electrician-avionics tech, but I can certainly add my name if you want an opinion about doing your own harness and/or tacking the job of installing all of the avionics and doing those 2 gazillion settings on your own.  Being able to buy both an AHRS and an autopilot from the same vendor is a big plus not available to me.  I have GRT stuff and I like it.  Besides buying mil spec wire, buying high grade teflon tape is a good idea too.

Terry
________________________________
To: reflector at tvbf.org<mailto:reflector at tvbf.org>
From: dtnelson at us.ibm.com<mailto:dtnelson at us.ibm.com>
Date: Sun, 30 Jun 2013 10:36:59 -0500
Subject: Re: REFLECTOR: Electrical system

Hi Reiff,

The power and ground bus bars I'm talking about is behind the canard bulkhead in the area behind the panel - not forward of the bulkhead and exposed.

In general, for exposed connections, the worry wouldn't be failure due to shorting from the water, it'd be corrosion.  In general, galvanic corrosion should be considered, but can be easily controlled with HW store electrician's grease.  The relays and connections that I do have on the forward (exposed) side of my bulkhead all have a dab of that stuff (main contactor, hydraulic pump relays, battery connections, etc.).

I've never seen galvanic corrosion on my homemade brass bus bars & the bimetal ring connectors I've used.

I've seen the other comments re. use of two alternators, etc. I agree with the guidance from Richard Gentil - if you've got an electrical problem you're going to want to land and fix it anyway.  Keeping your system as simple as possible and building your simple system with reliability in mind makes much more sense to me than trying to add all kinds of redundancy... which just gives Murphy more opportunities to ruin your day.  I'd think really hard before installing a system with two alternators, two batteries, all kinds of switching relays, lots of extra wiring... failure points... and things to go wrong.

My two cents.

Dave

Dave T. Nelson
T/L 553-4327, Voice 507-253-4327<tel:507-253-4327>, Fax 507-253-3648<tel:507-253-3648>
Program Director, ISC ECAT NPI & Test Engineering

Dave,

Terrific advice! Thanks for all the help.

Did you cover the power buss with anything? Is there any concern of having a "naked" power buss in the nose? I have an RG, so I'm imagining the entire inside of the nose will get wet if I take off or land in the rain.

I really appreciate all the info!

Reiff


From: reflector-bounces at tvbf.org<mailto:reflector-bounces at tvbf.org> [mailto:reflector-bounces at tvbf.org] On Behalf Of Dave T Nelson
Sent: Saturday, June 29, 2013 1:12 PM
To: reflector at tvbf.org<mailto:reflector at tvbf.org>
Subject: Re: REFLECTOR: Electrical system

This is an excellent area for KISS.... Keep It SIMPLE!

In my installation, I used two connection blocks in the area behind the instrument panel for both 12V and ground (4 total), one of each flavor on the left and on the right.  I made them myself by soldering brass screws into a brass plate.  I then used ring terminals on the wire ends.  The terminals are then held tight with MS21042 nuts.  The idea is to avoid having to have wires seeking 12V or ground from having to cross the whole panel from the left side to the right (or vise-versa).  The ground system should be simple - everything has only one grounding point (to avoid ground loops).  On both power and ground, the buss bars are powered (or grounded) via two wires for redundancy.

I used switch circuit breakers instead of switches with separate circuit breakers (or fuses).  I wouldn't recommend that... I've had a couple of them fail.

I used circuit breakers instead of fuses.  My reasoning was that I want to be able to see at a glance if one had popped (hard to do with a fuse).  I wish I'd used the type that allow you to pull the end of the circuit breaker to switch a circuit off.

Don't buy used circuit breakers!

Use real aviation grade wire, not Radioshack junk.

I used, carefully and religiously, a wire size chart.  I've seen many, many installations where folks use wire of way to low of a gauge (too thick and heavy).  You'll be surprised how often you can use 20 or even 22 gauge based on the current requirements.  Make sure the wiring chart you use is for bundled wire, not single strand.  Make sure you use the right size terminal for each wire.

I sized the circuit breakers for the load, not for the wire carrying capacity.  There has been some debate on this, as Nuckolls would size the fuse/circuit breaker for the wire, not the load.  IMHO I'm trying to protect the expensive load (radio), and the wire will always


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